CASCADE TECHNOLOGIES INC — National Aeronautics and Space Administration SBIR Phase I: A1

Description

<p style="margin-left:0in; margin-right:0in">Our long-term vision is to seamlessly integrate resolvent operator-based spectral analysis into Cascade&rsquo;s high-fidelity large eddy simulation (LES) environment, for accurate prediction and efficient modeling of supersonic jet noise from complex nozzles. Resolvent analysis is a frequency-domain technique that can identify resonance phenomena such as jet screech and other tonal acoustic effects, predict the large-scale coherent structures that are the main source of aft angle jet noise, and that provides, at the same time, sensitivity maps that can be used for optimal sensor or actuator placement for noise control. Cascade&rsquo;s LES framework features a novel mesh generation paradigm based on the computation of Voronoi diagrams, which allows for the generation of high-quality, body-fitted, conformal meshes and the use of low-dissipation numerical methods required for high fidelity large eddy simulations of multi-scale turbulent flows in complex geometries. We project that the combination of the Voronoi-based LES and resolvent analysis can be successfully commercialized by assuming a role similar to that of modal analysis in solid mechanics. In Phase I, we propose the case of a heated supersonic over-expanded turbulent jet issuing from a circular convergent-divergent nozzle as a testbed for both Cascade&rsquo;s Voronoi-based LES framework and a resolvent analysis tool provided by Caltech as a subcontractor. The first task is to implement and validate shock-capturing capabilities into both the resolvent tool and LES compressible flow solver &ldquo;Charles&rdquo;. Armed with the large-eddy simulation data, The second task is to conducte a detailed resolvent analysis of the over-expanded turbulent jet, with special emphasis on broadband aft angle and tonal shock-induced noise. In parallel, the final task is to perform a proof-of-concept simulation for an airframe-integrated nozzle, as a demonstration of the meshing and prediction capabilities for complex geometries.</p>